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Soyuz 11A511U-2
Part of R-7 Block I stage series Family
LOx/Kerosene propellant rocket stage. .

Status: In production.. Thrust: 298.10 kN (67,016 lbf). Gross mass: 25,200 kg (55,500 lb). Unfuelled mass: 2,355 kg (5,191 lb). Specific impulse: 330 s. Burn time: 250 s. Height: 6.74 m (22.11 ft). Diameter: 2.66 m (8.72 ft). Span: 2.66 m (8.72 ft).

Cost $ : 3.000 million.



Country: Russia. Engines: RD-0110. Launch Vehicles: Soyuz 11A511U / Ikar, Soyuz M, Soyuz 11A511U / Fregat. Propellants: Lox/Kerosene.

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